Knowledge of flow field behind lifting surfaces of supersonic airplane or missile is important in handling various stability problems; downwash and sidewash angles were measured with conical probe in vertical planes 0.5, 1.0 and 1.5 chord lengths downstream of rectangular wing of biconvex section.
Measurement of downwash and sidewash behind rectangular wing at mach number of 1.6
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 19 , n 5
1952
Article (Journal)
English
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Downwash and sidewash fields behind cruciform wings
NTRS | 1952
|Engineering Index Backfile | 1959
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